Method for reducing the freezing point of aminated aviation gasoline by the use of tertiaryamylphenylamine

ABSTRACT

A method is disclosed for reducing the freezing point of unleaded aminated aviation gasoline to −58° C. or lower by the addition of tert-amylphenylamine.

This application claims the benefit of U.S. Ser. No. 60/605,992 filedAug. 30, 2004.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to unleaded aviation gasoline of highmotor octane number, low deposit formation, non-fouling and a freezingpoint of −58° C. or lower, to an additive concentrate and to the methodfor producing the additive concentrate.

2. Description of the Related Art

The high octane requirements of aviation gas for use in piston drivenaircraft which operate under severe requirements, e.g., aircraftcontaining turbo-charged piston engines, require that commercialaviation fuels contain a high performance octane booster. The organicoctane boosters for automobile gasolines (Mogas) such as benzene,toluene, xylene, methyl tertiary butyl ether, ethanol, and the like, arenot capable by themselves of boosting the motor octane number (MON) tothe 98 to 100⁺ MON levels required for aviation gasolines (Avgas).Tetraethyl lead (TEL) is therefore a necessary component in high octaneAvgas as an octane booster.

Compositionally, Avgas is different from Mogas. Avgas, because of itshigher octane and stability requirements, is typically a blend ofisopentane, alkylate, toluene and tetraethyl lead. A typical Avgas basefuel without octane booster such as tetraethyl lead has a MON of 88 orhigher, typically 88 to 97. Mogas, which has lower octane requirements,is a blend of many components such as butane, virgin and rerun naphtha,light, intermediate and heavy cat naphthas, reformate, isomerate,hydrocrackate, alkylate and ethers, or alcohols. Octane requirements ofMogas are based on research octane numbers (RON). For a given fuel, theRON is on average 10 octane numbers higher than its corresponding MON.Thus, the average premium Mogas possesses a MON of 86 to 88, whereascurrent Avgas must have a MON of 99.5. MON, not RON, is the acceptedmeasure of octane for Avgas and is measured using ASTM D2700-92.

Conventional octane booster for Mogas, such as benzene, toluene, xylene,methyl tertiary butyl ether and ethanol are capable of boosting the MONof unleaded Avgas to the 92 to 95 MON range if added to Avgas in highenough concentrations. As noted previously, this is insufficient to meetthe needs of 98 MON high octane Avgas.

With the phasing out of tetra-ethyl lead as an octane booster resortmust be made to other means for boosting octane.

U.S. Pat. No. 5,470,358 teaches a high octane unleaded aviation gasolinecomprising unleaded aviation gasoline base fuel having a motor octanenumber of 90-93 and an amount of at least one aromatic amine effectiveto boost the motor octane number of the base fuel to at least about 98,the aromatic amine having the formula

wherein R₁ is C₁-C₁₀ alkyl, n is an integer of from zero to 3 with theproviso that R₁ cannot occupy the 2- or 6-position on the aromaticrings.

Alternatively the fuel can comprise the same base fuel and an amount ofat least one aromatic amine effective to boost the motor octane numberof the base fuel to at least 98, said aromatic amine being a halogensubstituted phenylamine or a mixed halogen and C₁-C₁₀ alkyl substitutedphenylamine again with the proviso that the alkyl group cannot occupythe 2- or 6-position on the phenyl ring.

Preferred halogens are Cl or F. When R₁ is alkyl, it occupies the 3-,4-, or 5- (meta or para) positions on the benzene ring. Alkyl groups inthe 2- or 6-position result in aromatic amines which cannot boost octaneto a MON value of 98. Examples of preferred aromatic amines for octaneimprovement include phenylamine, 4-tert-butylphenylamine,3-methylphenylamine, 3-ethylphenylamine, 4-methylphenylamine,3,5-dimethylphenylamine, 3,4-dimethylphenylamine,4-isopropylphenylamine, 2-fluorophenylamine, 3-fluorophenylamine,4-fluorophenylamine, 2-chlorophenylamine, 3-chlorophenylamine and4-chlorophenylamine. Especially preferred are 3,5-dimethylphenylamine,3,4-dimethylphenylamine, 2-fluorophenylamine, 4-fluorophenylamine,3-methylphenylamine, 3-ethylphenylamine, 4-ethylphenylamine,4-isopropylphenylamine and 4-t-butylphenylamine.

U.S. Pat. No. 5,851,241 and its continuation U.S. Pat. No. 6,258,134 aredirected to aviation fuel compositions which contain a combination of analkyl tertiary butyl ether, an aromatic amine and optionally a manganesecomponent such as methyl cyclopentadenyl manganese tricarbonyl (MMT).The base fuel to which the additive combination may be added may be awide boiling range alkylate base fuel. According to the patents thecombination of the alkyl tertiary butyl ether, the aromatic amine and,optionally, the manganese component result in a synergistic combinationwhile boosts the MON of the fuel to a degree greater than the sum of theMON increases for each additive when used individually in the base fuel.

Heretofore, the aromatic amines which have been investigated, whileexhibiting the ability to boost MON of aviation gasoline to 98 andhigher have also been found to be susceptible to fouling and depositformation and/or do not produce a fuel meeting the industry standard forfreezing point of −58° C. or lower.

It is desirable to find a way to reduce the freezing point of aviationgasoline preferably unleaded aviation gasoline to −58° C. and lower,avoid deposit formation and be non-fouling in aviation gasoline ofreduced toluene content while retaining high MON of at least 98.

DESCRIPTION OF THE FIGURES

FIG. 1 is a GC-FID trace of about 99.93% pure 4-tert-amylphenylamine.

FIG. 2 is a GC-FID trace of about 99.90% pure 4-tert-amylphenylamine.

FIG. 3 is a GC-FID trace of about 99.29% pure 4-tert-amylphenylamine.

DETAILED DESCRIPTION OF THE INVENTION

In accordance with the present invention, a method is provided forproducing an aminated aviation gasoline of at least 98 MON, low depositformation potential/non-fouling and reduced freezing point of at least−58° C. comprising adding to unleaded base aviation gasoline having aMON of at least 88 an effective amount of tert-amylphenylamine. Thetert-amylphenylamine (TAPA) employed is meta- and/orpara-tertiaryamylphenylamine, which also goes by the name 3- and/or 4-and/or 5-(1,1 dimethylpropyl)phenylamine, CAS #2049-92-5. When usedalone in the absence of any other octane booster, the amount oftert-amylpheylamine added to the fuel is an amount sufficient to boostthe octane of the aviation gasoline to at least 98 MON. The presentinvention is also directed to an additive concentrate useful for raisingthe MON of the aviation gasoline fuel to at least 98, reducing thefreezing point of the fuel to at least −58° C. and enabling the fuel toresist deposit formation and be non-fouling comprising thetert-amylphenylamine and at least one additional component selected froma carrier oil such as polypropylene oxide, an antioxidant, a detergent,toluene, and one or more other aromatic amine(s).

An amount of tert-amylphenylamine in the range of about 0.5 to up toabout 35 wt %, preferably about 1.0 to about 20 wt % more preferablyabout 1.0 to about 15 wt % can be used based on the total fuel.

The use of tert-amylphenylamine in unleaded aviation gasolinesurprisingly has been found to boost the MON of the fuel, to promoteresistance to deposit formation and fouling in the absence of addedsolvents such as toluene and yield a fuel having a freezing point of−58° C. and lower.

Fuels which freeze at −58° C. or which even exhibit some crystalformation at −58° C. are not considered as having a freezing point of−58° C. or less. The fuel must be substantially free of crystals at −58°C. in order to be considered as meeting the industry standard foraviation gasoline of having a freezing point of −58° C. or lower.

Crystal formation is determined by visual rating as described in ASTMD2386 Standard Test Method for Freezing Point of Aviation Fuels. A cloudforming at approximately −10° C. that does not grow in intensity is dueto water and may be disregarded (as per the ASTM D2386 method).

While tert-amylphenylamine can be employed by itself, it can also beemployed in combination with other aromatic amines such as those recitedin U.S. Pat. No. 5,470,358.

When used in combination with other such aromatic amines which alsoboost aviation gasoline MON, the tert-amylphenylamine is present in anyamount, e.g., at least about 15 mol % of the total of the aminespresent, preferably at least about 25 mol % of the total of the aminespresent, more preferably at least about 33 mol % of the total of theamines present, most preferably at least about 50 mol % of the total ofthe amines present, the tert-amylphenylamine being present in the fuelin the range previously recited, i.e., about 0.5 to up to about 35 wt %,preferably about 1.0 to about 20 wt %, more preferably about 1.0 to 15wt % based on the total fuel.

In blends where tert-amylphenylamine replaced at least half of thedifferent amine, e.g., t-butylphenylamine, the aminated aviationgasoline fuels containing such mixed amines had freezing points lowerthan −58° C. and were not supercooled at −58° C. As used herein, thephrase “not supercooled” defines a liquid which upon cooling to a giventemperature does not exhibit crystal formation, and upon warming stilldoes not exhibit crystal formation.

Generally the aminated aviation gasoline of the present inventioncontains anywhere from zero to up to about 25 wt % toluene, butpreferably is of very low toluene content, e.g., aminated aviationgasoline fuels containing zero to 6 wt % toluene, more preferably zeroto 2 wt % toluene, most preferably zero to <1.5 wt % toluene.

Toluene is used as a solvent and when used in high volume helps toreduce fouling and deposit formation in aminated fuel. When toluene isused or present in limited quantity when amines other thantert-amylphenylamine, t-butylphenylamine, or other alkylated phenylamines with no alpha hydrogen are used, fouling and deposit formationoccurs.

Even though some amines other than tert-amylphenylamine have been foundto lower the freezing point of aviation gasoline to −58° C. or less,such other amines require the use of substantial quantities of tolueneand/or detergent to limit fouling and deposit formation. In fuels whichhave low toluene and/or detergent content, however, such amines resultin measurable fouling and deposit formation.

Surprisingly, it has been found that tert-amylphenylamine not onlyboosts the MON of base aviation gasoline but also produces an aminatedaviation gasoline fuel having a freezing point of −58° C. or less whilepromoting resistance to fouling and deposit formation in lowtoluene/detergent content aminated aviation gasoline fuel.

The process of the present invention, therefore, finds particularutility in reducing the freezing point to −58° C. and less of aminatedaviation fuels which have very low toluene/detergent content aspreviously indicated.

Fouling and deposit formation are reduced by employing toluene. Toluenecontent of about 11 wt % and higher reduce or prevent fouling anddeposit formation. In the absence of toluene, however, evenisopropylphenylamine, which would produce an aminated aviation fuelhaving a freezing point of −58° C. or lower, is marked by fouling anddeposit formation.

By contrast, tert-amylphenylamine can be used to produce an aminatedaviation gasoline fuel having a freezing point of −58° C. and lower, anincreased MON and resistance to deposit formation and fouling, theaminated aviation gasoline containing no to very low toluene.

The base aviation gasoline to which the tert-amylphenylamine is addedmay also contain other additives. Examples of such additional additivesinclude TEL, carrier oils, antioxidants, detergents, toluene and dyes.Cosolvents can also be present and they can include low molecular weightaromatics, alcohols, nitrates, esters, ethers, halogenated hydrocarbonsand the like. With the phase out of TEL, other, conventional octaneboosters can be present, such as ethers, alcohols, and non-lead metals,including, e.g., ethyl tertiary butyl ether, methyl cyclopentadienylmanganese tricarbonyl, iron pentacarbonyl. Antioxidant content in thefuel can be up to 200 mg/liter of fuel, preferably up to 100 mg/liter offuel, more preferably up to 50 mg/liter of fuel, most preferably up to24 mg/liter of fuel. Detergent content in the fuel can be up to 1000ppm, preferably about 500 ppm, more preferably about 250 ppm, mostpreferably about 100 ppm. Carrier oil content in the fuel can be up to500 ppm, preferably up to 250 ppm, more preferably up to 100 ppm, mostpreferably up to 50 ppm. Approved additives for Avgas are listed in ASTMD-910.

The tert-amylphenylamine can be employed as a concentrate comprising thetert-amylphenylamine and at least one additional additive selected fromcarrier oil, antioxidant, detergent, toluene and one or more otheraromatic amine(s) as taught in U.S. Pat. No. 5,470,358, the amount ofany of those additional components in the additive concentrate beingsuch that upon addition of the concentrate to the base fuel in an amountsufficient to achieve a tert-amylphenylamine content in the resultingaminated aviation gasoline fuel of about 0.5 up to 35 wt % based thetotal aminated aviation gasoline fuel, preferably about 1.0 to about 20wt %, more preferably about 1.0 to 15 wt % based on total aminatedaviation gasoline fuel, the amount of said additional additive in theaminated aviation gasoline fuel is within the ranges recited above forthe particular additional additive(s).

4-tert-amylphenylamine can be synthesized by a number of routes, e.g.,the selective nitration of the hydrocarbon followed by the reduction tothe amine and vacuum distillation, the alkylation of aniline with theappropriate olefin using mild acid catalyst at temperatures of about200-250° C. followed by vacuum distillation.

The degree of final product purity may depend on the synthesis routetaken, routes which lead to the formation of byproducts being thoserequiring the higher degree of product purification.

Product from the alkylation of aniline can contain alkylatedchlorobenzene and/or alkylated nitro benzene and oxidation products asbyproducts, while product from the nitration of alkyl aromatichydrocarbon can contain oxidation products as well as isomers, dimersand diamine as byproducts.

The 4-tert-amylphenylamine used in the following examples was producedby the selective nitration of the alkyl aromatic hydrocarbon followed byreduction to the amine and vacuum distillation. Following thedistillation the recovered product had a measured purity of about 99.23%and about 99.29% for 2 assays. This product when added to base fuel wasof sufficient purity to give good deposits, fouling and freezing pointtest results but gave poor results in gum testing (ASTM D-873). When theproduct was redistilled under vacuum to a measured level of about 99.90%purity (one assay) the fuel to which it was added it still gave poorresults in gum testing (ASTM D-873) but when distilled under vacuum to ameasured level of about 99.93% purity the fuel to which it was addedgave good gum test results (i.e., low gum formation). The degree ofpurity of the preferred 4-tert-amylphenylamine for use in the presentinvention can be determined by Gas Chromatographic analysis (GC) astypically practiced by those skilled in the art.

The GC apparatus and procedure employed in generating the figurespresented herein are as follows: Instrument: Agilent 6890; Column: SGEHT-5 SIMD 0.1 μm 6 m×0.53 mm; Carrier gas: helium; flow rate: 8.4ml/min; Inlet Temperature: 430° C. (no-split); Oven: Initialtemperature: 30° C.; Initial Time: 0.0 min; Rate: 10° C./min; FinalTemperature: 430° C.; Final Time: 19 minutes; Detector: FID; DetectorTemperature: 430° C.

When subjected to such analysis, the preferred 4-tert-amylphenylaminewill produce a GC-FID trace substantially that of FIG. 1. Compare FIG. 1the GC-FID trace for the about 99.93% pure 4-tert-amylphenylamine withFIGS. 2 and 3. FIGS. 2 and 3 are the GC traces for the about 99.90% pureand the about 99.29% pure 4-tert-amylphenylamine respectively. Aspreviously stated, the materials of FIGS. 2 and 3 gave poor gum testresults. The closeness of the percent purity assays, however, indicatethat reliance merely on percent purity may not be sufficient to identifythe preferred material. It is believed that resort to the GC-FID traceis a better measure of the preferred material purity in the present casethan percent purity.

EXAMPLES Example 1

This example illustrates the effect on freezing point of the addition ofdifferent alkylphenylamines to alkylate aviation fuel. Blends in weight% Freeze Alkylate Alkylphenylamine Toluene Point in ° C. 89 11 4-TBPA 0−52 88 11 4-TBPA 1 −56 82 11 4-TBPA 6 pass*  90 0 4-TBPA 0 pass** 104-IPPA 89.5 5.5 4-TBPA 0 pass** 5 4-IPPA 95 5 4-TAPA 0 <−70 80 20 4-TAPA0 <−70*froze upon removal from cold bath at −59° C. (supercooled)**a few crystals formed on top of the sample upon warming Pass = −58° C.4-TBPA 4-tertiarybutylphenylamine4-IPPA 4-isopropylphenylamine4-TAPA 4-tert-amylphenylamine (material of FIG. 3)

Example 2

This example illustrates the effect on fouling and deposit formation ofthe addition of 4-t-butyl-, 4-isopropyl-, and 4-tert-amyl-phenylaminesto alkylate fuels. The test was run in accordance with the procedurereported in U.S. Pat. No. 5,492,005. In the test n-heptane insolublesand toluene insolubles were measured and the fouling potentialdetermined. In the test a metal nub is cycled between 150° C. and 300°C. in 9 minute cycles. About 40 ml of fuel is dripped on the nub in anair atmosphere. The nub is weighed before and after feed is dripped onit to five decimal places (0.00001 g). It is then washed with n-heptaneand weighed and with toluene and weighed to determine the n-heptane andtoluene insolubles. n-Heptane Toluene Feed to Deposit test insolubleinsoluble Fouling (all as wt %) deposit (mg) deposit (mg) Potential*alkylate 0 0 Non-fouling alkylate + 11% 0.08 0.08 Mildly fouling 4-TBPAalkylate + 11% 0.01 0.02 Non-fouling 4-TBPA + 11% toluene alkylate + 11%4-IPPA 0.14 0.14 Low-Moderate fouling alkylate + 11% + 4- 0.08 0.03Non-fouling IPPA 11% toluene alkylate + 12% 0.00 0.00 Non-fouling 4-TAPA(2 tests) (0.04) (0.03)*non-fouling is given as 0.03 mg or less deposit of toluene insolubles4-TBPA 4-tertbutylphenylamine4-IPPA 4-isopropylphenylamine4-TAPA 4-tert-amylphenylamine (material of FIG. 3)

Example 3

This example illustrates the effect on freezing point of the addition of4-tertamylphenylamine (99.29% purity, FIG. 3) and 4-t-butylphenylaminein different molar ratios to alkylate aviation fuel, at differentcooling temperatures. A total of between 11 wt % to about 12 wt % aminewas added to the alkylate then cooled either at −58° C. or −70° C. thenwarmed to room temperature. Cooled at −58° C. % of Amines ConcentrationLowest On Warming (molar) (wt %) Temperature Crystals Crystals 4-TAPA4-TBPA 4-TAPA 4-TBPA Reached (° C.) Appeared, ° C. Disappeared, ° C. 5050 6 5.5 −58 n/a n/a 25 75 3 8.2 −58 −54.5 −25 33 67 4 7.3 −58 −56.5−24.5 9 91 1.1 10 −41.5 −41.5 −20.5 0 100 0 11 −45 −45 −19.5 67 33 8 3.6−58 n/a n/a 75 25 9 2.8 −58 n/a n/a 90 10 10.8 1.1 −58 n/a n/a

Cooled at −70° C. % of Amines Concentration Lowest On Warming (molar)(wt %) Temperature T Crystals T Crystals 4-TAPA 4-TBPA 4-TAPA 4-TBPAReached (° C.) Appeared, ° C. Disappeared, ° C. 50 50 6 5.5 −67.5 −67.5−28 25 75 3 8.2 −69 −69 −24.5 33 67 4 7.3 −70 −2.5 −2.5 9 91 1.1 10−62.5 −62.5 −21.5 0 100 0 11 −58 −58 −16.5 5 95 0.6 10.4 −55.5 −55.5 −1767 33 8 3.6 −70 n/a n/a 75 25 9 2.8 −70 −50 −2.5 90 10 10.8 1.1 −70 n/an/a 0 100 0 11 −47.5 −47.5 −20.5

Example 4

This example illustrates the effect on the gum formation capacity ofaviation fuel containing 4-tert-amylphenylamines of different purities.

Each sample is a blend of 12 wt % 4-tert-amylphenylamine and 88 wt %alkylate. These blends were tested using the 16 hour version of ASTMD873. Purity of amine in 12 ASTM D873 16 hours Relative wt % TAPA/88 wt% Potential Gum Gum alkylate blend (mg/100 mL) Amount 99.29* 38.8 High99.90** 24.5 High 99.90** 22.1 High 99.93*** 6.4 Moderate 99.93*** 7.4Moderate*corresponds to FIG. 3**corresponds to FIG. 2***corresponds to FIG. 1

1. A method for reducing the freezing point of an aminated unleadedaviation gasoline to at least −58° C. comprising adding to base aviationgasoline having a MON of at least about 88 an effective amount of meta-and/or para-tert-amylphenylamine.
 2. The method of claim 1 wherein theaminated aviation gasoline has a very low toluene content.
 3. The methodof claim 2 wherein the aminated aviation gasoline contains from zero toabout 6 wt % toluene.
 4. The method of claim 2 wherein the aminatedaviation gasoline contains from zero to about 2 wt % toluene.
 5. Themethod of claim 2 wherein the aminated aviation gasoline contains fromzero to <1.5 wt % toluene.
 6. The method of claim 1, 2, 3, 4 or 5wherein the amount of tert-amylphenylamine added to the base aviationgasoline is in the range of about 0.5 to up to about 35 wt % based onthe total aminated aviation gasoline.
 7. The method of claim 6 whereinthe amount of tert-amylphenylamine added to the base aviation gasolineis in the range of about 1.0 to about 20 wt % based on the totalaminated aviation gasoline.
 8. The method of claim 6 wherein the amountof tert-amylphenylamine added to the base aviation gasoline is in therange of about 1.0 to about 15 wt % based on the total aminated aviationgasoline.
 9. The method of claim 1, 2, 3, 4 or 5 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 15 mol % of the total ofthe amines present.
 10. The method of claim 6 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 15 mol % of the total ofthe amines present.
 11. The method of claim 6 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 25 mol % of the total ofthe amines present.
 12. The method of claim 6 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 50 mol % of the total ofthe amines present.
 13. The method of claim 7 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 15 mol % of the total ofthe amines present.
 14. The method of claim 7 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 25 mol % of the total ofthe amines present.
 15. The method of claim 7 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 50 mol % of the total ofthe amines present.
 16. The method of claim 8 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 15 mol % of the total ofthe amines present.
 17. The method of claim 8 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitutes at least about 25 mol % of the total ofthe amines present.
 18. The method of claim 8 wherein the aminatedaviation gasoline contains one or more other alkylphenylamine octaneboosters in addition to the tert-amylphenylamine and wherein thetert-amylphenylamine constitute at least about 50 mol % of the total ofthe amines present.
 19. The method of claim 9 wherein thealkylphenylamine different than the tert-amylphenylamine has theformula:NH₂—Ar (R₁)_(n) wherein R₁ is selected from the group consisting ofC₁-C₁₀ alkyl, halogen and mixture thereof, Ar is a phenylene aromaticgroup, n is an integer from zero to 3 and wherein when n is 1 or 2 andwhen R₁ is alkyl it is in the meta- and/or para-position.
 20. Anadditive concentrate useful for producing an aminated aviation gasolinehaving a freezing point of −58° C. or lower comprising meta- and/orpara-tert-amylphenylamine and at least one of additional componentselected from carrier oil, antioxidant, detergent, toluene, and one ormore other aromatic amine(s).
 21. The additive concentrate of claim 20comprising tert-amylphenylamine and a carrier oil, the carrier oil beingpresent in the concentrate in an amount sufficient such that uponaddition of the concentrate to a base aviation gasoline to achieve atert-amylphenylamine content in the resulting aminated aviation gasolineof about 0.5 to up to about 35 wt % based on the total aminated aviationgasoline the concentrate contributes a carrier oil content of up to 500ppm carrier oil/liter of aminated aviation gasoline.
 22. The additiveconcentrate of claim 20 comprising tert-amylphenylamine and anantioxidant, the antioxidant being present in the concentrate in anamount sufficient such that upon addition of the concentrate to a baseaviation gasoline to achieve a tert-amylphenylamine content in theresulting aminated aviation gasoline of about 0.5 to up to about 35 wt %based on the total aminated aviation gasoline the concentratecontributes an antioxidant content of up to 200 mg antioxidant/liter ofaminated aviation gasoline.
 23. The additive concentrate of claim 20comprising tert-amylpheylamine and a detergent, the detergent beingpresent in the concentrate in an amount sufficient that upon addition ofthe concentrate to a base aviation gasoline to achieve atert-amylphenylamine content in the resulting aminated aviation gasolineof about 0.5 to up to about 35 wt % based on the total aminated aviationgasoline the concentrate contributes a detergent content of up to about1000 ppm detergent/liter of aminated aviation gasoline.
 24. The additiveconcentrate of claim 20 comprising tert-amylphenylamine and toluene, thetoluene being present in the concentrate in an amount sufficient suchthat upon addition of the concentrate to a base aviation gasoline toachieve a tert-amylphenylamine content in the resulting aminatedaviation gasoline of about 0.5 to up to about 35 wt % based on the totalaminated aviation gasoline, the concentrate contributes a toluenecontent of up to 25 wt % of the aminated aviation gasoline.
 25. Theadditive concentrate of claim 20 comprising tert-amylphenylamine and oneor more other aromatic amines wherein the other aromatic amineconstitutes up to 85 mol % of the total of the mixture of aminespresent.
 26. The additive concentrate of claim 25 additionallycontaining an antioxidant in an amount sufficient such that, uponaddition of the concentrate to a base aviation gasoline to achieve atert-amylphenylamine content in the resulting aminated aviation gasolineof about 0.5 to up to about 35 wt % based on the total aminated aviationgasoline, the antioxidant content of the aminated aviation gasoline isup to 200 mg antioxidant/liter of aminated aviation gasoline.
 27. Theadditive concentrate of claim 25 additionally containing a detergent inan amount sufficient such that, upon addition of the concentrate to abase aviation gasoline to achieve a tert-amylphenylamine content in theresulting aminated aviation gasoline of about 0.5 to up to about 35 wt %based on the total aminated aviation gasoline, the detergent content ofthe aminated aviation gasoline is up to about 1000 ppm detergent/literof aminated aviation gasoline.
 28. The additive concentrate of claim 25additionally containing toluene in an amount sufficient such that uponaddition of the concentrate to a base aviation gasoline to achieve atert-amylphenylamine content in the resulting aminated aviation gasolineof about 0.5 to up to about 35 wt % based on total aminated aviationgasoline the toluene content of the aminated aviation gasoline is up toabout 25 wt %.
 29. The additive concentrate of claim 25 additionallycontaining a carrier oil in an amount sufficient such that upon additionof the concentrate to a base aviation gasoline to achieve atert-amylphenylamine component in the resulting aminated aviationgasoline of about 0.5 to up to about 35 wt % based on total aminatedaviation gasoline, the carrier oil content of the aminated aviationgasoline is up to 500 ppm carrier oil/liter of aminated aviationgasoline.
 30. The additive concentrate of claim 25 additionallycontaining a detergent and an antioxidant in an amount sufficient suchthat upon addition of the concentrate to a base aviation gasoline toachieve a tert-amylphenylamine content in the aminated aviation gasolineof about 0.5 to up to about 35 wt % based on total aminated aviationgasoline, the detergent and antioxidant content of the aminated aviationgasoline is up to about 1000 ppm detergent/liter of aminated aviationgasoline and up to 200 mg antioxidant/liter of aminated aviationgasoline.
 31. The additive concentrate of claim 26, 27, 28 or 30additionally containing a carrier oil in an amount sufficient such thatupon addition of the concentrate to a base aviation gasoline to achievea tert-amylphenylamine content in the resulting aminated aviationgasoline of about 0.5 to up to about 35 wt % based on total aminatedaviation gasoline, the carrier oil content of the aminated aviationgasoline is up to 500 ppm carrier oil/liter of aminated aviationgasoline.
 32. The additive concentrate of claim 20 comprisingtert-amylphenylamine, an antioxidant, and a detergent, the antioxidantand the detergent being present in the concentrate in an amountsufficient that upon addition of the concentrate to a base aviationgasoline to achieve a tert-amylphenylamine content in the resultingaminated aviation gasoline of up to 35 wt % based on the total aminatedaviation gasoline the antioxidant and detergent content of the aminatedaviation gasoline is up to 200 mg antioxidant/liter of aminated aviationgasoline and up to 1000 ppm detergent/liter of aminated aviationgasoline.
 33. The additive concentrate of claim 20 comprisingtert-amylphenylamine, an antioxidant, a detergent, and a carrier oil,the antioxidant, detergent, and carrier oil being present in theconcentration in an amount sufficient such that upon addition of theconcentration to a base aviation gasoline to achieve atert-amylphenylamine content in the resulting aminated aviation gasolineof about 0.5 to up to 35 wt % based on the total aminated aviationgasoline, the antioxidant, detergent and carrier oil content of theaminated aviation gasoline is up to 200 mg antioxidant/liter of aminatedaviation gasoline, up to 1000 ppm detergent/liter of aminated aviationgasoline, and up to 500 ppm carrier oil/liter of aminated aviationgasoline.
 34. The additive concentrate of claim 26, 27, 29, 30, 32 or 33additionally containing toluene in an amount sufficient such that uponaddition of the concentrate to a base aminated aviation gasoline toachieve a tert-amylphenylamine content in the resulting aminatedaviation gasoline of about 0.5 to up to about 35 wt % based on the totalaminated aviation gasoline the toluene content of the aminated aviationgasoline is up to about 25 wt %.
 35. The additive concentrate of claim31 additionally containing toluene in an amount sufficient such thatupon addition of the concentrate to a base aviation gasoline to achievea tert-amylphenylamine content in the resulting aminated aviationgasoline of about 0.5 to up to about 35 wt % based on the total aminatedaviation gasoline the toluene content of the fuel is up to about 25 wt%.
 36. A method for producing an additive concentrate, said concentratebeing useful for lowering the freezing point of aminated aviationgasoline comprising mixing meta- and/or para-tert-amylphenylamine withat least one additional additive selected from carrier oil, antioxidant,detergent, toluene and one or more other aromatic anines.
 37. The use ofthe concentrate of claim 20 in a base aviation gasoline fuel in anamount sufficient to achieve a freezing point of −58° C. or lower.